Invention Grant
- Patent Title: Configuring and positioning air passage holes in a combustion chamber wall
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Application No.: US16850114Application Date: 2020-04-16
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Publication No.: US11441779B2Publication Date: 2022-09-13
- Inventor: François Pierre Ribassin , Patrice André Commaret , Romain Nicolas Lunel , Christophe Pieussergues
- Applicant: Safran Aircraft Engines
- Applicant Address: FR Paris
- Assignee: Safran Aircraft Engines
- Current Assignee: Safran Aircraft Engines
- Current Assignee Address: FR Paris
- Agency: Blank Rome LLP
- Priority: FR1904171 20190418
- Main IPC: F23R3/04
- IPC: F23R3/04

Abstract:
The provision of air passage holes through a wall of a gas turbomachine combustion chamber. Multi-perforations are virtually positioned and distributed, even in a first safety zone without air passage openings. Multi-perforations with a virtual inlet or outlet in this first security zone are virtually removed. According to certain criteria, at least some of said removed multi-perforations are then virtually reintegrated, and, from then on a perimeter passing through the virtual inlets and outlets of all the multi-perforations present is defined, in the direction of a primary or dilution hole to be installed, a modified safety zone is defined, then, respecting around said hole and with the freedom to reposition it within this limit, the shape of this hole is redefined.
Public/Granted literature
- US20200333008A1 CONFIGURING AND POSITIONING AIR PASSAGE HOLES IN A COMBUSTION CHAMBER WALL Public/Granted day:2020-10-22
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